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The mechanical properties and Lankford coefficients of AA6061-T6 sheets, calculated from the uniaxial tension test in the rolling direction are presented in Table 1. Hill’s 1948 yield criterion was used to describe the plastic and anisotropic behavior of the
middle part of the aluminum alloy sheet whose thickness is 12 mm. And the residual stress decreases largely after stretching. The elimination effect of residual stress varies with
the analysis of stretch forming over the punch head remained unsolved. Intensive analyses of sheet metal forming have been presented by many authors. Elastic-plastic [2], elastic
A7.1 Conventional and High-Strength Aluminum Alloys. Both 2000 and 7000 series aluminum alloys are used in the aerospace/aircraft industry. Ta-. bles A7.1 and A7.2
In this work, formabilities of aluminum sheet alloy grade AA5052-H32 were investigated under consideration of the anisotropic behavior of material. Experimental
sheets and the damage is more at high coefficient of friction, strains-rate and temperature. (Minoru Yamashita et al [7, 8]) led formability tests to examine on impact of strain-rate
Simulated and experimental investigation of stretch sheet forming of commercial AA1200 aluminum alloy. AA1200 aluminum alloy; sheet forming;
Stretch forming shapes aluminum sheets and extrusion profiles into simple or complex contoured curves with tensile and bending forces. The material is kept under
Fabrication of Aluminium. Aluminium alloys are normally supplied as semi-finished products such as sheet, plate, coil, extrusions, tube or wire. All forms can then be